Multi-objective six sigma approach applied to robust airfoil design for mars airplane

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2007, Pages 3261-3270

  Shimoyama, Koji ^a,b,d   Oyama, Akira ^c,d,e   Fujii, Kozo ^c,d,e  

^a UNIVERSITY OF TOKYO   (Japan)

^b TOHOKU UNIVERSITY   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d Institute of Fluid Science ^*

^e JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MACH NUMBER; MACHINE DESIGN; OPTIMIZATION;

CURVATURES; PARAMETER TUNING; PITCHING MOMENT;

AIRFOILS;

EID: 34547564177     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-1966     Document Type: Conference Paper

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